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Find the eigenvalues and eigenvectors of the following matrices.\(\left(\begin{array}{rrr}-3 & 2 & 2 \\ 2 & 1 & 3 \\ 2 & 3 & 1\end{array}\right)\)

Short Answer

Expert verified
Solve the characteristic polynomial for eigenvalues. Then, for each eigenvalue, solve \((A - \lambda_i I)x = 0\) for eigenvectors.

Step by step solution

01

- Set Up Characteristic Equation

To find the eigenvalues of matrix \(A\), first calculate the characteristic polynomial. The characteristic polynomial is given by the determinant equation \( \det(A - \lambda I) = 0 \), where \( \lambda \) represents the eigenvalues and \(I\) is the identity matrix.
02

- Substitute Matrix and Identity Matrix

Substitute the given matrix \(A\) and the identity matrix \(I\) into the equation: \[A - \lambda I = \begin{pmatrix}-3 & 2 & 2 \ 2 & 1 & 3 \ 2 & 3 & 1\end{pmatrix} - \lambda \begin{pmatrix}1 & 0 & 0 \ 0 & 1 & 0 \ 0 & 0 & 1\end{pmatrix} = \begin{pmatrix}-3 - \lambda & 2 & 2 \ 2 & 1 - \lambda & 3 \ 2 & 3 & 1 - \lambda\end{pmatrix}\].
03

- Compute the Determinant

Evaluate the determinant of the resulting matrix to get the characteristic polynomial. Compute \(\det(\begin{pmatrix}-3 - \lambda & 2 & 2 \ 2 & 1 - \lambda & 3 \ 2 & 3 & 1 - \lambda\end{pmatrix})\).
04

- Solve for Eigenvalues

Solve the characteristic polynomial equation for \( \lambda \). This will give you the eigenvalues of the matrix. The determinant calculation yields the polynomial equation:\[(-(3+\lambda))((1-\lambda)((1-\lambda)) - 9) - 2((4-3\lambda) - 8) + 2((3-9) - 2(-\lambda+3)) = 0\].Simplifying, we get the polynomial \[ -\lambda^3 + \lambda^2 + 10\lambda - 22 = 0\].This equation can be solved to find the eigenvalues.
05

- Find Eigenvectors

For each eigenvalue \( \lambda_i \), solve the equation \((A - \lambda_i I)x = 0\) to find the eigenvector associated with \( \lambda_i \). For example, if \( \lambda_1 = 2 \), substitute \( \lambda_1 \) into \(A - \lambda_1 I\) and solve for vector \(x\). Repeat this process for each eigenvalue.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Characteristic Polynomial
In linear algebra, a **characteristic polynomial** plays a crucial role in finding eigenvalues of a matrix. To derive the characteristic polynomial, you need to set up the characteristic equation given by \(\det(A - \lambda I) = 0 \), where \(A\) is your given matrix and \(\lambda \) represents the eigenvalues you seek. Here, \(I\) is an identity matrix—essentially a matrix in which all diagonal elements are 1 and all off-diagonal elements are 0.
To form the characteristic polynomial, subtract \(\lambda I\) from the given matrix \(A\), and calculate the determinant of the result. This determinant becomes the characteristic polynomial you solve for the eigenvalues.
For our given example, the matrix \(A\) is \(\begin{pmatrix}-3 & 2 & 2 \ 2 & 1 & 3 \ 2 & 3 & 1\textbackslashend{pmatrix}\) and the identity matrix \(I\) is \(\begin{pmatrix}1 & 0 & 0 \ 0 & 1 & 0 \ 0 & 0 & 1\textbackslashend{pmatrix}\). Calculate \(A - \lambda I\), and then find the determinant.
Determinant
The **determinant** of a matrix is a scalar value that can tell us if a matrix is invertible and is used in numerous calculations in linear algebra. To find the eigenvalues, you need to calculate the determinant of the matrix \(A - \lambda I\).
For our matrix \(A\), after substituting and simplifying, we get: \(\begin{pmatrix}-3 - \lambda & 2 & 2 \ 2 & 1 - \lambda & 3 \ 2 & 3 & 1 - \lambda \textbackslashend{pmatrix}\).
The next step is to compute the determinant of this matrix, which involves expanding along any row or column. The simplified form of \(\textbackslash det (A - \lambda I)\) gives us a polynomial in \(\lambda \), known as the characteristic polynomial. In our case, it simplifies to \(-\lambda^3 + \lambda^2 + 10\lambda - 22 = 0 \).
Matrix Algebra
In **matrix algebra**, operations like addition, subtraction, and finding determinants are essential. It's the foundation for solving systems of linear equations and performing transformations.
When you work with eigenvalues and eigenvectors, you often need to manipulate matrices. For example, given the matrix \(A\), you create another matrix by subtracting \(\lambda I\) and then calculate the determinant.
Once you have the characteristic polynomial, solving it gives you the eigenvalues. Each eigenvalue corresponds to a specific transformation described by the matrix \(A\). For our matrix, the polynomial \(-\lambda^3 + \lambda^2 + 10\lambda - 22 = 0\) reveals the eigenvalues upon solving.
Linear Equations
To find the **eigenvectors**, you need to solve systems of **linear equations**. Given each eigenvalue \( \lambda_i \), you form a new matrix \(A - \lambda_i I \).
By setting up the equation \( (A - \lambda_i I)x = 0 \), where \(x \) is the eigenvector, you solve for \( x \). This is essentially solving a homogeneous system of linear equations.
For each eigenvalue from the polynomial \(-\lambda^3 + \lambda^2 + 10\lambda - 22 = 0 \), substitute back into \(A - \lambda_i I \) and solve. This gives you the eigenvectors. For example, if \( \lambda_1 = 2 \), plug it into \(A - 2I \) and solve the resulting system to find the corresponding eigenvector. Repeat this for all eigenvalues.

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Most popular questions from this chapter

Show that the product \(A A^{\mathrm{T}}\) is a symmetric matrix.

Let each of the following matrices \(M\) describe a deformation of the \((x, y)\) plane. For each given \(M\) find: the eigenvalues and eigenvectors of the transformation, the matrix \(C\) which diagonalizes \(M\) and specifies the rotation to new axes \(\left(x^{\prime}, y^{\prime}\right)\) along the eigenvectors, and the matrix \(D\) which gives the deformation relative to the new axes. Describe the deformation relative to the new axes.\(\left(\begin{array}{rr}2 & -1 \\ -1 & 2\end{array}\right)\)

Find the "distance"' between the " points "? \(\begin{array}{ll}\text { (a) }(4,-1,2,7) & \text { and }(2,3,1,9) ; \\ \text { (b) }(-1,5,-3,2,4) & \text { and }(2,6,2,7,6)\end{array}\)

(a) If a body is rotating about a fixed axis, then its angular momentum \(L\) and its angular velocity \(\boldsymbol{o}\) are parallel vectors and \(\mathrm{L}=\mathrm{le} \mathrm{s}\), where \(I\) is the (scalar) moment of inertia of the body about the axis. However, in general, \(L\) and \(\omega\) are not parallel and \(I\) in the equation must be a second-order tensor; let us call it I. Find I in dyadic form in the following way: For simplicity, first consider a point mass \(m\) at the point \(r\). The angular momentum of \(m\) about the origin is by definition \(m r \times v\), where \(v\) is the linear velocity.From Chapter \(6, v=\omega \times r .\) Write out the triple vector product for \(L\) and from it write each component of \(\mathrm{L}\) in terms of the three components of 6 . Write your results in matrix form and in dyadic form $$ \mathbf{L}=\mathbf{I} \cdot \mathbf{\omega}=\left(\mathrm{ii} l_{x x}+\mathrm{ij} l_{x y}+\cdots\right)+\omega $$ You should have $$ I_{x z}=m\left(y^{2}+z^{2}\right), \quad I_{x y}=-m x y, \quad \text { etc. } $$ For a set of masses \(m_{i}\) or an extended body, replace the cxpressions for \(I_{z x+}, \operatorname{ctc}_{4}\), by the corresponding sums or integrals: $$ \begin{aligned} &I_{x x}=\sum m_{i}\left(y_{i}^{2}+z_{i}^{2}\right) \quad \text { or } \quad \int\left(y^{2}+z^{2}\right) d m_{4} \\ &I_{x y}=-\sum m_{j} x_{i} y_{i} \quad \text { or }-\int x y d m_{4} \quad \text { etc. } \end{aligned} $$ (b) Show that 1 is a second-order (Cartesian) tensor by expressing its components relative to a rotated system \(\left[I_{s^{\prime} x^{\prime}}=m\left(y^{2}+z^{\prime 2}\right)\right.\), etc. \(]\) in terms of \(x, y, z\) using \((11.7)\) or \((11.11)\), and hence in terms of \(I_{x \pi}\), etc., to show that I obeys the transformation equations \((11,13)\). (c) Show that if \(\mathrm{n}\) is a unit vector, the expression \(\mathbf{n}+\mathbf{1} \cdot \mathbf{n}\) gives the moment of inertia about an axis through the origin parallel to n. Hint: Consider I rotated to a system in which one of the axes is along \(n\). (d) Observe that the I matrix is symmetric and recall that a symmetric matrix may be diagonalized by a rotation of axes. The eigenvalues of the I matrix are called the principal moments of inertia. Show by part (c) that they are moments of inertia abour the new axes \(\left(x^{\prime}, y^{\prime}, z^{\prime}\right)\) relative to which \(\mathbf{I}\) is diagonal. These new axes are called the principal axes of incrtia. For the mass distribution consisting of point masses \(m\) at \((1,1,1)\) and \((1,1,-1)\), find the nine components of 1, and find the principal moments of inertia and the principal axes.

The characteristic equation for a second-order matrix \(M\) is a quadratic equation. We have, considered in detail the case in which \(M\) is a real symmetric matrix and the roots of thecharacteristic equation (eigenvalues) are real, positive, and unequal. Discuss some other possibilities as follows: (a) \(M\) real and symmetric, eigenvalues real, one positive and one negative. Show that the plane is reflected in one of the cigenvector lines (as well as stretched or shrunk). Consider as a simple special case $$ M=\left(\begin{array}{rr} 1 & 0 \\ 0 & -1 \end{array}\right) $$ (b) \(M\) real and symmetric, eigenvalues equal (and therefore real). Show that \(M\) must he a multiple of the unit matrix. Thus show that the deformation consists of dilation or shrinkage in the radial direction (the same in all directions) with no rotation (and reflection in the origin if the root is negative). (c) \(M\) real, not symmetric, eigenvalues real and not equal. Show that in this case the eigenvectors are not orthogonal. Hint: Find their dot product. (d) \(M\) real, not symmetric, eigenvalues complex, Show that all vectors are rotated, that is, there are no (real) eigenvectors which are unchanged in direction by the transformation. Consider the characteristic equation of a rotation matrix as a special case.

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